Bristol Aquila

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Aquila
BristolAquila.JPG
Type Piston aircraft engine
Manufacturer Bristol Aeroplane Company
First run 1934
Major applications Bristol Bulldog
Bristol Bullpup

The Aquila was a nine-cylinder single-row radial aircraft engine designed by the Bristol Engine Company starting in 1934. A sleeve valve engine, its basic design was developed from the Bristol Perseus. The Aquila was never used in production, but further developments led to the Bristol Hercules, Bristol Taurus, and Bristol Centaurus.[1]

Design and development[edit]

The Aquila was developed two years after the somewhat larger Perseus, both being sleeve valve designs. The primary difference was in size, the Perseus was based on the 5.75 by 6.5 in (146 by 165 mm) cylinder used in the Mercury engine, while the Aquila used a new and smaller 5 by 5.375 in (127.0 by 136.5 mm) sized cylinder. The result was a reduction in displacement from 1520 to 950 cubic inches (24.9 to 15.6 L).

The first Aquila engine delivered a modest 365 horsepower (272 kW), which was hardly spectacular for an engine of this size. It soon developed into more powerful versions as improvements were worked into the line (as well as similar changes to the Perseus), and by 1936 it had improved to 500 hp (370 kW). This would have made it an excellent replacement for the Bristol Jupiter, which ended production at 590 hp (440 kW) three years earlier, but by this time almost all interest was on ever-larger engines.

Applications[edit]

Note:[2]

Specifications (Aquila I)[edit]

Data from Lumsden.[3]

General characteristics

  • Type: Nine-cylinder single-row naturally aspirated air-cooled radial engine
  • Bore: 5 in (130 mm)
  • Stroke: 5.375 in (136.5 mm)
  • Displacement: 950 cu in (15.6 L)
  • Length: 41 in (1,000 mm)
  • Diameter: 46 in (1,200 mm)
  • Dry weight: 776 pounds (352 kg)

Components

Performance

See also[edit]

Related development
Related lists

References[edit]

Notes[edit]

  1. ^ Gunston 1989, p.33.
  2. ^ List from Lumsden, the Bulldog and Bullpup were test aircraft only.
  3. ^ Lumsden 2003, p.118.

Bibliography[edit]

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.